ADVISORY CIRCULAR - Federal Aviation …

1 AC 120-27E DATE: 6/10/05 ADVISORY CIRCULAR AIRCRAFT weight AND BALANCE CONTROL Flight Standards Service Washington, Initiated By: AFS-200/AFS-300 Subject: AIRCRAFT weight AND BALANCE CONTROL Date: 6/10/05 Initiated By: AFS-200/AFS-300 AC No: 120-27E Change: 1. What is the purpose of this ADVISORY CIRCULAR (AC)? a. This AC provides operators with guidance on how to develop and receive approval for a weight and balance control program for aircraft operated under Title 14 of the Code of Federal Regulations (14 CFR) part 91, subpart K of part 91, and parts 121, 125, and 135. b. This AC presents recommendations for an acceptable means, but not the only means, to develop and receive approval for a weight and balance control program, and includes guidance for using average and estimated weights in accordance with part 121, section (b) and other applicable parts of subpart K of part 91 and parts 121, 125, and 135.

2 NOTE: Per part 125, section (b), no person may operate an airplane in a part 125 operation unless the current empty weight and center of gravity (CG) are calculated from the values established by an actual weighing of the airplane within the preceding 36 calendar-months. c. If an operator adopts the suggestions contained in this AC, the operator must ensure that, when appropriate, it replaces discretionary language such as should and may with mandatory language in relevant manuals, operations specifications (OpSpecs), or management specifications (MSpecs). 2. How is this AC organized? This AC has three main chapters and six appendixes. Chapter 1 addresses aircraft weighing and loading schedules.

3 Chapter 2 describes different methods to determine the weight of passengers and bags. Chapter 3 addresses the Federal Aviation Administration s (FAA) role in developing and approving an operator s weight and balance control program. Finally, Appendixes 1 through 6 contain technical information such as definitions, sources of data used in the AC, a sample loading envelope, an additional curtailment for passenger weight variation, suggestions to improve accuracy, and a checklist for operators. AC 120-27E 6/10/05 3. What documents does this AC cancel? This AC cancels AC 120-27D, Aircraft weight and Balance Control, dated August 11, 2004. 4. What should an operator consider while reading this AC?

4 A. Accurately calculating an aircraft s weight and CG before flight is essential to comply with the certification limits established for the aircraft. These limits include both weight and CG limits. By complying with these limits and operating under the procedures established by the manufacturer, an operator is able to meet the weight and balance requirements specified in the aircraft flight manual (AFM). Typically, an operator calculates takeoff weight by adding the operational empty weight (OEW) of the aircraft, the weight of the passenger, cargo payload, and the weight of fuel. The objective is to calculate the takeoff weight and CG of an aircraft as accurately as possible. b.

5 When using average weights for passengers and bags, the operator must be vigilant to ensure that the weight and balance control program reflects the reality of aircraft loading. The FAA will periodically review the guidance in this AC and update this AC if average weights of the traveling public should change or if regulatory requirements for carry-on bags or personal items should change. Ultimately, the operator is responsible for determining if the procedures described in this AC are appropriate for use in its type of operation. 5. Who should use this AC? a. This document provides guidance to both passenger and cargo operators that are either required to have an approved weight and balance control program under parts 121 and 125, or choose to use actual or average aircraft, passenger, or baggage weights when operating under part 91, subpart K of part 91, or part 135.

6 The guidance in this AC is useful for anyone involved in developing or implementing a weight and balance control program. b. As shown in table 1, the FAA has divided aircraft into three categories for this AC to provide guidance appropriate to the size of the aircraft. table 1. AIRCRAFT CABIN SIZE For this AC, an aircraft originally type-certificated with Is considered 71 or more passenger seats A large-cabin aircraft. 30 to 70 passenger seats A medium-cabin aircraft. 5 to 29 passenger seats A small-cabin aircraft. NOTE: Aircraft with fewer than five passenger seats must use actual passenger and baggage weights. 6. Who can use standard average or segmented weights? a. Standard Average Weights.

7 Use of standard average weights is limited to operators of multiengine turbine-powered aircraft originally type-certificated for five or more passenger seats Page ii 6/10/05 AC 120-27E who hold a letter of authorization (LOA), OpSpecs, or MSpecs, as applicable, and were certificated under 14 CFR part 25, 29, or part 23 commuter category or the operator and manufacturer is able to prove that the aircraft can meet the performance requirements prescribed by part 23 commuter category aircraft.

8 Single-engine and multiengine turbine Emergency Medical Service Helicopter (EMS/H) operators may use standard average weights for EMS operations, provided they have received an LOA. b. Segmented Weights. Segmented weights are provided for, but not limited to those aircraft that are multiengine turbine-powered aircraft originally type-certificated for five or more passenger seats and that do not meet the performance requirements of part 23 commuter category aircraft or part 29. Segmented passenger weights are listed in Chapter 2, table 2-5. c. The FAA s recommendations and advice on the safe use of standard average weights and segmented weights are contained in this document. In the FAA s view, it would be unsafe for an aircraft operator to use standard average weights or segmented weights in any of the following aircraft: (1) All single-engine piston-powered aircraft.

9 (2) All multiengine piston-powered aircraft. (3) All turbine-powered single-engine aircraft. NOTE: All multiengine turbine-powered aircraft certificated under part 23, except for commuter category aircraft, may only use an actual weight or segmented weight program. Operators that elect to use a segmented weight program must meet the requirements in paragraph 6b and curtail the CG envelope as specified in Appendix 3, 4, and 5. Commuter category aircraft may use standard average weights and should refer to paragraph 200f for further guidance. 7. When will the FAA revise the standard average weights in this AC? The FAA will periodically review the standard average passenger weights listed in this AC, after the release of a new National Health and Nutrition Examination Survey (NHANES).

10 (For information on NHANES, see Appendix 2.) If the FAA finds that the data from NHANES indicates a weight change of more than 2 percent, the FAA will revise this AC to update the standard average weights. /s/ John M. Allen for James J. Ballough Director, Flight Standards Service Page iii AC 120-27E 6/10/05 [THIS PAGE INTENTIONALLY LEFT BLANK] Page iv 6/10/05 AC 120-27E table OF CONTENTS Paragraph Page CHAPTER 1.